1. Hang X, Fei Q, Su W. On Tracking Aeroelastic Modes in Stability Analysis Using Left and Right Eigenvectors[J]. AIAA Journal, 2019, 57(10): 4447–4457.
2. Hang X, Fei Q, Su W, Jiang D. Analytical Sensitivity Analysis of Flexible Aircrafts with the Unsteady Vortex-Lattice Aerodynamic Theory[J]. Aerospace Science and Technology, 2020, 99(1): 105612-105612.
3. 杭晓晨,蒋令闻,顾明华,吴邵庆,费庆国.频域分解模态识别方法的阻尼识别精度研究[J].振动工程学报,2015,28(04):518-524.
| 4. Hang X, Fei Q, Su W. A Mode Tracking Method in Aeroelastic Stability Analysis Using Left Eigenvectors[C].2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. 2018: 1204.
5. Wang M, Hang X. Modified Micro-Mechanics Based Multiscale Model for Damage Analysis of Open-Hole Composite Laminates under Compression[J]. Materials, 2022, 15(15): 5105.
6. Zhou Y, Hang X, Wu S, et al. Frequency-dependent random fatigue of panel-type structures made of ceramic matrix composites[J]. Acta Mechanica Solida Sinica, 2017, 30(2): 165-173.
| 7. Zhu R, Fei Q, Jiang D, Hang X. Using Sherman–Morrison theory to remove the coupled effects of multi-transducers in vibration test[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2019, 233(4): 1364-1376.
8. 薛程,李彦斌,杭晓晨等.复合材料机翼热气弹剪裁研究及分析系统研发[J].东南大学学报(自然科学版),2022,52(05):899-906.
| 9. 朱锐,杭晓晨,姜东,费庆国,靳文冰.基于奇异值分解的ERA改进算法及模态定阶[J].振动.测试与诊断,2018,38(01):115-122+210.
| 10. 蒋令闻,杭晓晨,费庆国.基于正交检验法的颤振分析模态跟踪技术[J].振动与冲击,2017,36(19):84-89+134.
| 11. 王燕,杭晓晨,姜东,韩晓林,费庆国.协方差驱动随机子空间的Toeplitz矩阵行数选择方法[J].振动与冲击,2015,34(07):71-75+92.
|
|
| (1) 费庆国; 杭晓晨; 李彦斌; 姜东; 蒋令闻 ; 一种用于机翼颤振分析的特征值追踪方法, 2020-3-19, 中国, ZL202010194840.1
|
|
